2. Fuel in Combustion chamber Turbine Net Power Air in Out Axial compressor Centrifugal compressor Exhaust Figure 1 Figure 1 shows the basic gas turbine cycle. Calculate the efficiency of the system if the temperature for the condition showed in T-s diagram below. Take that mass flow rate is 23 kg/s and the Cp is 35.5 J. K-l mol-". TA 8913 °C- 3 4987 °C 2 4665 °C- 1276 °C

2. Fuel in Combustion chamber Turbine Net Power Air in Out Axial compressor Centrifugal compressor Exhaust Figure 1 Figure 1 shows the basic gas turbine cycle. Calculate the efficiency of the system if the temperature for the condition showed in T-s diagram below. Take that mass flow rate is 23 kg/s and the Cp is 35.5 J. K-l mol-". TA 8913 °C- 3 4987 °C 2 4665 °C- 1276 °C

Elements Of Electromagnetics

7th Edition

ISBN:9780190698614

Author:Sadiku, Matthew N. O.

Publisher:Sadiku, Matthew N. O.

ChapterMA: Math Assessment

Section: Chapter Questions

Problem 1.1MA

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